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用于三电极负载的固态脉冲电源设计

Solid state pulse power supply design for three-electrode load
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摘要 设计了一种基于Marx的三电极脉冲电源。采用磁环隔离驱动方案和双MOSFET驱动电路,实现了在三电极负载下同时输出正负高压脉冲。分析了电路的运行方式,搭建了32级脉冲电源,并设计了一种针板电极和DBD电极结合的三电极负载,实现了总输出电压13 kV,脉宽10μs,频率1 kHz,且输出电压、脉宽可调。实验验证了该电源方案在三电极负载下的可行性。 A three-electrode pulse power supply based on Marx is designed.Magnetic ring isolation driving scheme and dual MOSFET driving circuit are adopted to realize the simultaneous output of positive and negative high-voltage pulses under the three-electrode load.Firstly,the operation mode of the circuit was analyzed,a 32-stage pulse power supply was built,and a three-electrode load combined with the pin-plate electrode and DBD electrode was designed.The total output voltage is 13 kV,the pulse width is 10μs,and the frequency is 1 kHz.Meanwhile,the output voltage and the pulse width are adjustable.The feasibility of the proposed power supply scheme under the three-electrode load is verified by experiments.
作者 郭凯 师国杰 黄利飞 GUO Kai;SHI Guojie;HUANG Lifei(School of Mechanical Engineering,University of Shanghai for Science and Technology,Shanghai 200093,China)
出处 《农业装备与车辆工程》 2023年第4期84-88,共5页 Agricultural Equipment & Vehicle Engineering
关键词 三电极 介质阻挡放电 等离子体 脉冲电源 脉冲功率技术 three electrodes dielectric barrier discharge plasma pulse power supply pulse power technology
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  • 1Webb N, Clifford C, Samimy M. Control of oblique shock wave/boundary layer interactions using plasma actuators[J]. Experiments in Fluids. 2013, 54(6): 1545.
  • 2Emerick T, Ali M Y, Foster C, et al. SparkJet characterizations in quiescent and supersonic flowfields[J]. Experiments in Fluids, 2014, 55(12): 1858.
  • 3Mamunuru M, Guo S, Poon D, et al. Separation control using plasma actuator: "simulation of plasma actuator[R]. San Antonio, Texas: AIAA, 2009.
  • 4Jukes T N, Choi K, Johnson G A, et al. Turbulent drag reduction by surface plasma through spanwise flow oscillation[R]. San Francisco, California: AIAA, 2006.
  • 5Roupassov D V, Zavyalov I N, Starikovskii A Y, et al. Boundary layer separation plasma control using low-temperature non-equilibrium plasma of gas discharge[R]. Reno, Nevada: AIAA, 2006.
  • 6Debien A, Benard N, Moreau E. Streamer inhibition for improving force and electric wind produced by DBD actuators[J]. Journal of Physics D: Applied Physics, 2012, 44(21): 215201.
  • 7Popkin S H, Taylor T M, Cybyk B Z. Development and application of the plasma synthetic jet actuator for high-speed flow control[J]. Johns Hopkins APL Technical Digest, 2013, 32( 1): 404-419.
  • 8Belinger A, Hardy P, Barricau P, et al. Influence of the energy dissipation rate in the discharge of a plasma synthetic jet actuator[J]. Journal of Physics D: Applied Physics, 2011,44(36):365201.
  • 9Cybyk B Z, Wilkerson J T, Grossman K R, et al. Computionalassessment of the sparkjet flow control actuator[R]. Reno, Nevada: AIAA, 2003.
  • 10Cybyk B Z, Grossman K R, Wilkerson J T, et al. Single-pulsed performance of the SparkJet flow control actuator[R]. Reno, Nevada: AIAA, 2005.

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